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Old   June 30, 2015, 14:33
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Oleg
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Hi guys. As I see this topic is still being viewed, but mainly for the geometry. Several people have already asked me about it so I decided to update the link. Here is the fresh link to my google drive.
https://drive.google.com/folderview?...0k&usp=sharing

Hope this'll help. Good luck!
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Old   November 3, 2015, 20:58
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Armando E. Kitto
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Thanks, olegmang!
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Old   December 24, 2015, 03:11
Default axial compressor stage 37 (rotor and stator) turbogrid curves
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manju
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Hi
I am working on subsonic axial compressor stage 37 (rotor and stator) turbo-grid curves files.i have the data of stage 37 blade coordinates,i have rotor 37 blade coordinates.csv file of hub,shroud and blade profile and its matching no of blades in rotor is 36
currently i am facing problem in stator turbo-grid coordinates.i am unable to create hub.curve,shroud.curve and blade profile .curve,
if anyone having turbogrid curve files for stage pls send it,no of blade in stator is 46,
journal which i am working
Design and Overall Performance
of Four Highly Loaded, High-Speed
Inlet Stages for an Advanced
High-Pressure-Ratio Core Compressor,Lonnie Reid and Royce D. Moore
Lewis Research Center
Cleveland, Ohio stage page 44-51,stage 37,
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Old   April 25, 2016, 04:24
Default nasa 37 stage turbogrid mesh files.gtm file
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manju
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Hi friends,i have done stage 37 mesh using turbogrid,
mesh of stator is fine,but when i use rotor 37 .i am getting -ve volume.can you guys pls send me the mesh file of rotor and stator 37.
i.e gtm file
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Old   May 23, 2016, 12:20
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mohammad
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Dear all
I need the geometry of NASA axial compressor stage 36 & 38 , If you have stage36 or38 geometry's data, wish u could share them with me

geometry cad file or geometry excel file.

i have a problem in geometry of both them.when i draw stage 36 & 38 ,some sketch look wrong.but i dont know why.

please help me.

email : mohammad_est@yahoo.com
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Old   October 12, 2016, 14:41
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Zoi
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Quote:
Originally Posted by olegmang View Post
In fact, I have coordinates in more convenient format for you (see attached). I've already extracted them from turbogrids rotor for each section and put into separate .txt files that you can easily import to SolidWorks and then loft a surface.
Hello. I know it's been a while since this thread was active, but could you tell me how you moved from turbogrid back to profile across the blade's span please? Thanks
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